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An overview of rotorcraft propulsion research at Lewis Research CenterRotorcraft propulsion research at Lewis Research Center is discussed, stressing programs in four areas of component research: compressors, combustors, turbines and transmissions, and three developmental programs: the Small Turboshaft Engine Research (STER) Project, the Advanced Rotorcraft Transmission (ART) program, and the Compound Cycle Engine (CCE) program. The component research emphasizes special problems of turboshaft engines in the 5 lb/sec to 30 lb/sec range. The objectives of the STER program are to evaluate the application of advanced concepts to small turboshaft engine systems and to investigate system related phenomena, such as distortion effects and secondary flow phenomena. The goals of the ART program are to reduce transmission weight by 25 percent, noise generation by 10 dB and mean time between removal to 5,000 hrs. The CCE program is working to combine the airflow capacity and light-weight features of a gas turbine with the more efficient, but heavier diesel turbine.
Document ID
19880053327
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Bill, Robert C.
(NASA Lewis Research Center Cleveland, OH, United States)
Weden, Gilbert J.
(NASA Lewis Research Center; U.S. Army, Propulsion Directorate, Cleveland OH, United States)
Coy, John J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 13, 2013
Publication Date
June 1, 1988
Publication Information
Publication: Vertiflite
Volume: 34
ISSN: 0042-4455
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
ISSN: 0042-4455
Accession Number
88A40554
Distribution Limits
Public
Copyright
Other

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